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Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63
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- http://id.worldcat.org/fast/1004756
- http://id.loc.gov/authorities/subjects/sh85079305
- http://id.loc.gov/authorities/subjects/sh85130657
- http://id.worldcat.org/fast/965814
- http://id.loc.gov/authorities/subjects/sh85063718
- http://id.loc.gov/authorities/subjects/sh85001297
- http://id.worldcat.org/fast/798221
- http://id.worldcat.org/fast/1139019
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- "Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63"
- "Experimental and theoretical aerodynamic characteristics of two hypersonic cruise aircraft concepts at Mach numbers of 2.96, 3.96, and 4.63"@en